A method for adjusting the path of a satellite to limit a risk of collision with items of debris each having a date of closest pass with the satellite is disclosed including: propagating at least one orbit from the reference path of the satellite according to at least one manoeuvre to the farthest date of closest pass; determining a probability of collision for each item of debris according to the at least one orbit; determining at least one overall probability according to the set of probabilities determined; selecting the lowest overall probability from among the at least one overall probability obtained; determining a command for the satellite including the manoeuvre associated with the lowest overall probability.


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    Title :

    PROCÉDÉ D'AJUSTEMENT DE TRAJECTOIRE ORBITALE DE SATELLITE


    Additional title:

    METHOD FOR ADJUSTING THE ORBITAL PATH OF A SATELLITE
    VERFAHREN ZUR EINSTELLUNG DER UMLAUFBAHN EINES SATELLITEN


    Contributors:

    Publication date :

    2023-10-25


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    French


    Classification :

    IPC:    B64G Raumfahrt , COSMONAUTICS



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